What was found
THREE CR3212-5-10 CHERRY FASTENERS SHEARED AT THE ATTACHMENT POINT OF THE BLOCK AND TUBE IN THE FLAP SYSTEM. FLAPS WERE SELECTED ON LANDING WITH NO RESPONSE. THIS IS A HIGH-TIME TRAINING AIRCRAFT.
- Difficulty date
- March 5, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N101CM
- Make and model
- Beech A24R
- Aircraft serial
- MC146
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Block
- Part number
- 1695240249
- Condition
- Rivets Sheared
- Location
- Flap Tube
- Part time
- 4,848 hours
- Stage of operation
- AP
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.